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Division [9A108] Components, other than those specified in 9A008, as follows, specially designed for solid and hybrid rocket propulsion systems:F1

Changes not yet applied. Later legislation changes this provision in ways not yet written into the text below:

  1. a..

    Rocket motor cases and "insulation" components therefor, usable in subsystems specified in 9A007, 9A009, 9A107 or 9A109.a.;

  2. b..

    Rocket nozzles, usable in subsystems specified in 9A007, 9A009, 9A107 or 9A109.a.;

  3. c..

    Thrust vector control sub-systems, usable in "missiles".

    Technical Note:

    Examples of methods of achieving thrust vector control specified in 9A108.c. are:

    1. 1..

      Flexible nozzle;

    2. 2..

      Fluid or secondary gas injection;

    3. 3..

      Movable engine or nozzle;

    4. 4..

      Deflection of exhaust gas stream (jet vanes or probes); or

    5. 5..

      Thrust tabs.

Annotations

Textual amendments

F1

Substituted by Commission Delegated Regulation (EU) 2020/1749 of 7 October 2020 amending Council Regulation (EC) No 428/2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items.